Interactive 3D Orbit Visualizer

Explore orbital mechanics by adjusting the classical Keplerian elements in real time. Simulate satellite trajectories around the Earth or the Moon, and visualize physical vectors and reference planes.

Earth Orbit

Drag to rotate • Scroll to zoom • Right-click to pan

Orbital Telemetry

Orbit Type Elliptical

Orbit Period 1.63 hrs

Velocity 7.58 km/s

Escape Velocity 10.72 km/s

Apoapsis Altitude 500 km

Periapsis Altitude 500 km

Keplerian Elements

Periapsis Altitude (h_p) 500 km

Eccentricity (e) 0.000

Inclination (i) 28.5°

RAAN (Ω) 0.0°

Argument of Periapsis (ω) 0.0°

Time Warp 100x

Visualizations & Body

Central Gravity Field

Equatorial Plane VNC Reference Vectors